US2420153A - Flexible exhaust conduit assembly - Google Patents
Flexible exhaust conduit assembly Download PDFInfo
- Publication number
- US2420153A US2420153A US512744A US51274443A US2420153A US 2420153 A US2420153 A US 2420153A US 512744 A US512744 A US 512744A US 51274443 A US51274443 A US 51274443A US 2420153 A US2420153 A US 2420153A
- Authority
- US
- United States
- Prior art keywords
- tubing
- flex
- collar
- flex tubing
- metal
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L11/00—Hoses, i.e. flexible pipes
- F16L11/14—Hoses, i.e. flexible pipes made of rigid material, e.g. metal or hard plastics
- F16L11/16—Hoses, i.e. flexible pipes made of rigid material, e.g. metal or hard plastics wound from profiled strips or bands
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N2470/00—Structure or shape of gas passages, pipes or tubes
- F01N2470/06—Tubes being formed by assembly of stamped or otherwise deformed sheet-metal
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N2470/00—Structure or shape of gas passages, pipes or tubes
- F01N2470/12—Tubes being corrugated
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T403/00—Joints and connections
- Y10T403/45—Flexibly connected rigid members
- Y10T403/453—Flexible sleeve-type coupling
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T403/00—Joints and connections
- Y10T403/47—Molded joint
- Y10T403/477—Fusion bond, e.g., weld, etc.
Definitions
- An object of the invention is to provide a strong and leak-proof joint between a length of flex tubing and a terminal fitting therefor.
- a more specific object is to provide a strong, leak-proof and durable welded joint between a piece of flex tubing and a terminal fitting therefor.
- Flex tubing constructed of some heat and corrosion-resistant material, such as stainless steel or inconel, is very well adapted for making connections between relatively movable parts of the exhaust system of an aeroplane, because of its free flexing characteristics.
- difiiculty has been-encountered in joining the ends ofthe flex tubing to the associated parts of the exhaust system.
- it has been attempted to attach flex tubing to a terminalfitting by providing on the latter a sleeve which telescopically engaged the flex tubing and then welding or brazing the overlapping end portion of the flex tubing to the sleeve.
- the flex tubing Because of the fact that the end portion of the flex tubing is sandwiched between the relatively heavy terminal fitting and collar, the flex tubing is protected from the welding flame so that it is not excessively heated and melted before the metal of the terminal fitting and of the collar is fused, and the molten metal of the weld bonds thoroughly with the metal of the flex tube adjacent the end thereof.
- Fig. 1 is a side elevation view of a flexible exhaust hose assembly in accordance with themvention
- Fig. 2 is a detail longitudinal section throughone of the weld connections of Fig. 1 the view showing a form of flex tubing having a packin therein;
- Fig. 3 is a detail section similar to Fig. 2 but showing a flex member having no packing
- Fig. 4 is a perspective view showing how the welded joint of Figs. 1, 2 and 3 is made.
- a short section Ill of flex' tubing having secured to its opposite ends a pair of terminal fittings I l and I2, respectively.
- the flex tubing l0 may be of standard construction in which a thin, rather narrow ribbon of metal is folded and rolled into a helix ofoverlapping interlocking turns.
- the shape of the ribbon employed in a packed hose may be as shown in Fig. 2 in which a packing I3 is rolled with the formed ribbon.
- the shape of the ribbon in a hose having no packing may be as shown in Fig. 3.
- the terminal fittings may be of various shapes, according to the design of the structure of which the flex tubing forms a part.
- the terminal connection I I has a flange M which may be bolted to a cooperating flange on an element to which the connection is to be attached.
- the weld metal I! is solidly fused to the surface portion of the nipple I5 and with the outer edge of the collar I6 and flows in and about and is fused to the thin metal of the flex tubing.
- a convenient method of forming the joint just described is to first position the collar IS on the end of the flex tubing I0 and then insert the nipple I5.
- the collar I6 may be temporarily secured to the end of the flex tubing by spot welding it thereto as indicated at I-8, several spots being made at circumferentially spaced points, or the collar may be so dimensioned as to fit snu ly on the flex tubing and thereby remain in posi-v tion.
- the weld can be formed with a welding flame I9 and a weld rod as illustrated in Fig. 4 in which the welding operation proceeds from right to left. It will be observed from Fig. 4 that although the thin edge ll of the flex tubing does not completely fill the space between the nipple I5 and the collar I6, it is nevertheless protected from excessive heating by the flame I9 because of its proximity to the heavier members I5 and I8 so that the edge does not burn away but remains intact during the welding operation and is solidly bonded to the weld metal I].
- the tubular section I 5 and the external sleeve I6 are all preferably'formed of the same material, which may be stainless steel or inconel.
- the additional weld metal supplied by the rod 20 is preferably of the same material.
- the material of the flex tubing may vary in thickness but is usually approximately .020" thick.
- the nipple I5 and the collar I6 should be of thicker material and it has been found that very satisfactory Joints result when these members are approximately .050" thick.
- ture of the terminal fitting is that it connect to the flex tubing by means of a nipple extending thereinto.
- the flex tubing might consist of a plurality of individual rings instead of a continuous helical strip.
- a flexible conduit assembly comprising: a section of flexible metal tubing consisting of interlocking turns of thin sheet metal; a terminal'fltting having a metal-nipple telescoped within the end portion of said tubing and of substantially greater thickness than said thin sheet metal 01' said tubing; ametal collar also of substantially greater thickness than said-thin sheet metal and surrounding the end portion of said tubing, the outer end of said collar being substantially flush with the end of said tubing; and an annular fillet of weld metal extending from said nipple to said collar and fused to said nipple, collar and tubin at least said tubing and fillet being of metal having the same fusing temperature.
Description
May 6, 1947. H. A. SPRENGER EI'AL 2,420,153 I FLEXIBLE EXHAUST CONDUIT ASSEMBLY Filed Dec. s, 1943 INVENTORS HAROLD A.SPRENGER BY m JOSEPH R. GREENE ATTORN EY.
Patented May 6, 1947 w EXHAUST CONDUIT ASSEMBLY Harold A. Sprenger and Joseph B. Greene, San
Diego, Calif., assignors to Solar Aircraft Company, San Diego, Calif., a corporation of California Application December 3, 1943, Serial No. 512,744
1 Claim. (01. 285-72) 1 This invention relates to flexible exhaust conduits for aircraft engines and particularly to exhaust conduits of the type consisting of a helical metal strip having overlapping interlocking turns and commonly referred to as flex tubing.
An object of the invention is to provide a strong and leak-proof joint between a length of flex tubing and a terminal fitting therefor.
A more specific object is to provide a strong, leak-proof and durable welded joint between a piece of flex tubing and a terminal fitting therefor.
Other more specific objects and features of the invention will appear from the detailed description to follow of a particular embodiment of the invention.
Flex tubing constructed of some heat and corrosion-resistant material, such as stainless steel or inconel, is very well adapted for making connections between relatively movable parts of the exhaust system of an aeroplane, because of its free flexing characteristics. However, difiiculty has been-encountered in joining the ends ofthe flex tubing to the associated parts of the exhaust system. Heretofore it has been attempted to attach flex tubing to a terminalfitting by providing on the latter a sleeve which telescopically engaged the flex tubing and then welding or brazing the overlapping end portion of the flex tubing to the sleeve. However, difficulty was encountered due tothe relative thinness of the flex tubing material, the material burning or melting back a substantial distance from the end when the flame was applied thereto, this melting back occurring before the heavier material of the telescoping sleeve could be raised to the fusing temperature. Attempts have been made to prevent this destruction of the thin flex tubing material by. employing brazing metals or alloys having substantially lower fusing temperatures than the tubing material, but this did not satisfactorily solve the problem. In the first place, it did not entirely eliminate excessive burning back of the flex tube material and, in the second place, the joint produced by the brazing materials was not as satisfactory under high operating temperatures as a true weld.
In accordance with the present invention, we easily obtain a strong and leak-proof weld connection between flex tubing and a sleeve terminal connection therefor by providing an additional short sleeve on the opposite side of the flex tube from the terminal connection. Thus, it is usually desirable to telescope the terminal fitting within the flex tubing, and in such construction we provide an additional short sleeve or collar surrounding the flex tubing at the end thereof and then weld the end edges of the external collar and the flex tubing to the exterior surface of the terminal fitting. Because of the fact that the end portion of the flex tubing is sandwiched between the relatively heavy terminal fitting and collar, the flex tubing is protected from the welding flame so that it is not excessively heated and melted before the metal of the terminal fitting and of the collar is fused, and the molten metal of the weld bonds thoroughly with the metal of the flex tube adjacent the end thereof.
In the drawing: t
Fig. 1 is a side elevation view of a flexible exhaust hose assembly in accordance with themvention;
Fig. 2 is a detail longitudinal section throughone of the weld connections of Fig. 1 the view showing a form of flex tubing having a packin therein;
Fig. 3 is a detail section similar to Fig. 2 but showing a flex member having no packing; and
Fig. 4 is a perspective view showing how the welded joint of Figs. 1, 2 and 3 is made.
Referring first to Fig. 1, thereis shown a short section Ill of flex' tubing having secured to its opposite ends a pair of terminal fittings I l and I2, respectively.
The flex tubing l0 may be of standard construction in which a thin, rather narrow ribbon of metal is folded and rolled into a helix ofoverlapping interlocking turns. The shape of the ribbon employed in a packed hose may be as shown in Fig. 2 in which a packing I3 is rolled with the formed ribbon. The shape of the ribbon in a hose having no packing may be as shown in Fig. 3. These types of flex tubing do not constitute a part of the present invention.
The terminal fittings may be of various shapes, according to the design of the structure of which the flex tubing forms a part. In Fig. 1, the terminal connection I I has a flange M which may be bolted to a cooperating flange on an element to which the connection is to be attached. The terthe end of the flex tube I0 and to a collar l6,
which surrounds the flex tubing and has its outer end approximately flush with the end of the flex tubing. As shown in Figs. 2 and 3, the weld metal I! is solidly fused to the surface portion of the nipple I5 and with the outer edge of the collar I6 and flows in and about and is fused to the thin metal of the flex tubing.
A convenient method of forming the joint just described is to first position the collar IS on the end of the flex tubing I0 and then insert the nipple I5. The collar I6 may be temporarily secured to the end of the flex tubing by spot welding it thereto as indicated at I-8, several spots being made at circumferentially spaced points, or the collar may be so dimensioned as to fit snu ly on the flex tubing and thereby remain in posi-v tion. It is desirable to secure the collar to the flex tubing in some manner to insure that at the time the weld is made, the end of the flex tubing will either be flush with or will project slightly beyond the end of the collar I6, in order to insure a bondbetween the weld metal and the flex tubing at all circumferential points.
After the collar It has been mounted on the flex tubing Ill and the nipple It has been inserted, the weld can be formed with a welding flame I9 and a weld rod as illustrated in Fig. 4 in which the welding operation proceeds from right to left. It will be observed from Fig. 4 that although the thin edge ll of the flex tubing does not completely fill the space between the nipple I5 and the collar I6, it is nevertheless protected from excessive heating by the flame I9 because of its proximity to the heavier members I5 and I8 so that the edge does not burn away but remains intact during the welding operation and is solidly bonded to the weld metal I].
In exhaust structures for aeroplanes and the like the flex tubing III, the tubular section I 5 and the external sleeve I6 are all preferably'formed of the same material, which may be stainless steel or inconel. Likewise, the additional weld metal supplied by the rod 20 is preferably of the same material.
The material of the flex tubing may vary in thickness but is usually approximately .020" thick. The nipple I5 and the collar I6 should be of thicker material and it has been found that very satisfactory Joints result when these members are approximately .050" thick.
It is to be specifically understood that the invention is not limited to use with the particular terminal fittings shown in the drawing, those servlishingCo. (Copy available in Div. 14, p. 517.)!
ture of the terminal fitting is that it connect to the flex tubing by means of a nipple extending thereinto.
Other variations and departures from the exact construction shown and described can be made without departing from the invention which is to be limited only to the extent set forth in the appended claim'. For example, the flex tubing might consist of a plurality of individual rings instead of a continuous helical strip.
We claim:
A flexible conduit assembly comprising: a section of flexible metal tubing consisting of interlocking turns of thin sheet metal; a terminal'fltting having a metal-nipple telescoped within the end portion of said tubing and of substantially greater thickness than said thin sheet metal 01' said tubing; ametal collar also of substantially greater thickness than said-thin sheet metal and surrounding the end portion of said tubing, the outer end of said collar being substantially flush with the end of said tubing; and an annular fillet of weld metal extending from said nipple to said collar and fused to said nipple, collar and tubin at least said tubing and fillet being of metal having the same fusing temperature.
' HAROLD A. SPRENGER.
JOSEPH R. GREENE.
Rarammcas crran The following references are of record in the file of this patent: V
UNITED STATES PATENTS Number Name I Date 2,240,413 Parker Apr. 29, 1941 1,340,813 Brinkman May 18, 1920 1,684,554 Riefen'stahl Sept, 18, 1928 1,129,979 Hewitt et al Mar. 2, 1915 1,939,242 Thaheld Dec. 12, 1933 2,040,140 Kidd May 12, 1938 2,322,924 Daiger June 29, 1943 FOREIGN PATENTS Number Country Date 356,921 French 1905 12,482 British May 20, 1914 OTHER REFERENCES Publication: The Welding Encyclopedia-Tenth Edition, published by Th Welding Engineer Pub-
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US512744A US2420153A (en) | 1943-12-03 | 1943-12-03 | Flexible exhaust conduit assembly |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US512744A US2420153A (en) | 1943-12-03 | 1943-12-03 | Flexible exhaust conduit assembly |
Publications (1)
Publication Number | Publication Date |
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US2420153A true US2420153A (en) | 1947-05-06 |
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ID=24040375
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US512744A Expired - Lifetime US2420153A (en) | 1943-12-03 | 1943-12-03 | Flexible exhaust conduit assembly |
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Cited By (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2832613A (en) * | 1954-06-10 | 1958-04-29 | Flexonics Corp | Autogenous welded laminated expansion joint for conduits |
DE4130739A1 (en) * | 1991-08-08 | 1993-02-11 | Witzenmann Metallschlauchfab | METAL WRAP HOSE |
US5362113A (en) * | 1992-09-02 | 1994-11-08 | Tru-Flex Metal Hose Corp. | Spot-welded end fitting for flexible metal piping |
US5494319A (en) * | 1994-06-06 | 1996-02-27 | Tru-Flex Metal Hose Corporation | Sleeved flexible metal piping, method of manufacturing same and flue system application of same |
US5538294A (en) * | 1994-11-01 | 1996-07-23 | Tru-Flex Metal Hose Corporation | Corrugated flexible metal piping assembly |
US5720504A (en) * | 1996-03-29 | 1998-02-24 | Dormont Manufacturing Company | Convoluted fluid connector assembly with hardened end portion |
US5741029A (en) * | 1996-02-14 | 1998-04-21 | Tru-Flex Metal Hose Corporation | Piping adapter |
US6102446A (en) * | 1999-02-06 | 2000-08-15 | Tru-Flex Metal Hose Corporation | Polygonal flexible metal hose coupling assembly |
US6311736B2 (en) | 1998-05-28 | 2001-11-06 | Donaldson Company, Inc. | Flexible hose and method for manufacturing |
US6312021B1 (en) | 1996-01-26 | 2001-11-06 | Tru-Flex Metal Hose Corp. | End-slotted flexible metal hose |
US6341805B1 (en) * | 1998-03-17 | 2002-01-29 | Tru-Flex Metal Hose Corp | Vehicle exhaust system with improved pipe end configurations |
US6508277B1 (en) * | 1999-07-27 | 2003-01-21 | Donaldson Company, Inc. | Flexible pipe with compressed ends |
US6513552B1 (en) * | 2001-09-28 | 2003-02-04 | General Machinery Of Pittsburgh, Inc. | Multi-flex stainless steel roof drain hose |
US6742815B2 (en) | 2002-05-08 | 2004-06-01 | Dormont Manufacturing Company | Fluid line connector assembly |
US20080283328A1 (en) * | 2007-05-18 | 2008-11-20 | International Truck Intellectual Property Company, Llc | Longitudinal stringer exhaust flex pipe assembly |
US9273810B1 (en) * | 2012-02-14 | 2016-03-01 | Delafield Corporation | Metal hose fitting and flanged insert that safely conducts high velocity fluids/gases up to Mach 1 |
USD756872S1 (en) | 2014-11-20 | 2016-05-24 | Stauffer Diesel, Inc. | Exhaust pipe |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR356921A (en) * | 1905-08-12 | 1905-12-13 | Manuf Metallurg De La Jonchere | Flexible metal hose |
US1129979A (en) * | 1912-08-29 | 1915-03-02 | Herbert H Hewitt | Hose-coupling. |
GB191412482A (en) * | 1914-05-20 | 1915-04-08 | William Henry Kanzow Bowley | Improvements in Flexible Metallic Tubing. |
US1340818A (en) * | 1916-09-11 | 1920-05-18 | Titeflex Metal Hose Corp | Flexible tube |
US1684554A (en) * | 1926-06-23 | 1928-09-18 | Degussa | Protective sheath for flexible shafts |
US1939242A (en) * | 1932-02-15 | 1933-12-12 | Guiberson Diesel Engine Compan | Coupling |
US2040140A (en) * | 1934-08-01 | 1936-05-12 | Kellogg M W Co | Method of welding tubular connecters |
US2240413A (en) * | 1939-09-09 | 1941-04-29 | Arthur L Parker | Coupling |
US2322924A (en) * | 1940-02-05 | 1943-06-29 | Hoover Co | Method of making motors |
-
1943
- 1943-12-03 US US512744A patent/US2420153A/en not_active Expired - Lifetime
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR356921A (en) * | 1905-08-12 | 1905-12-13 | Manuf Metallurg De La Jonchere | Flexible metal hose |
US1129979A (en) * | 1912-08-29 | 1915-03-02 | Herbert H Hewitt | Hose-coupling. |
GB191412482A (en) * | 1914-05-20 | 1915-04-08 | William Henry Kanzow Bowley | Improvements in Flexible Metallic Tubing. |
US1340818A (en) * | 1916-09-11 | 1920-05-18 | Titeflex Metal Hose Corp | Flexible tube |
US1684554A (en) * | 1926-06-23 | 1928-09-18 | Degussa | Protective sheath for flexible shafts |
US1939242A (en) * | 1932-02-15 | 1933-12-12 | Guiberson Diesel Engine Compan | Coupling |
US2040140A (en) * | 1934-08-01 | 1936-05-12 | Kellogg M W Co | Method of welding tubular connecters |
US2240413A (en) * | 1939-09-09 | 1941-04-29 | Arthur L Parker | Coupling |
US2322924A (en) * | 1940-02-05 | 1943-06-29 | Hoover Co | Method of making motors |
Cited By (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2832613A (en) * | 1954-06-10 | 1958-04-29 | Flexonics Corp | Autogenous welded laminated expansion joint for conduits |
DE4130739A1 (en) * | 1991-08-08 | 1993-02-11 | Witzenmann Metallschlauchfab | METAL WRAP HOSE |
US5362113A (en) * | 1992-09-02 | 1994-11-08 | Tru-Flex Metal Hose Corp. | Spot-welded end fitting for flexible metal piping |
US5494319A (en) * | 1994-06-06 | 1996-02-27 | Tru-Flex Metal Hose Corporation | Sleeved flexible metal piping, method of manufacturing same and flue system application of same |
US5538294A (en) * | 1994-11-01 | 1996-07-23 | Tru-Flex Metal Hose Corporation | Corrugated flexible metal piping assembly |
US6312021B1 (en) | 1996-01-26 | 2001-11-06 | Tru-Flex Metal Hose Corp. | End-slotted flexible metal hose |
US5741029A (en) * | 1996-02-14 | 1998-04-21 | Tru-Flex Metal Hose Corporation | Piping adapter |
US5720504A (en) * | 1996-03-29 | 1998-02-24 | Dormont Manufacturing Company | Convoluted fluid connector assembly with hardened end portion |
US6341805B1 (en) * | 1998-03-17 | 2002-01-29 | Tru-Flex Metal Hose Corp | Vehicle exhaust system with improved pipe end configurations |
US6311736B2 (en) | 1998-05-28 | 2001-11-06 | Donaldson Company, Inc. | Flexible hose and method for manufacturing |
US6102446A (en) * | 1999-02-06 | 2000-08-15 | Tru-Flex Metal Hose Corporation | Polygonal flexible metal hose coupling assembly |
US6508277B1 (en) * | 1999-07-27 | 2003-01-21 | Donaldson Company, Inc. | Flexible pipe with compressed ends |
US6513552B1 (en) * | 2001-09-28 | 2003-02-04 | General Machinery Of Pittsburgh, Inc. | Multi-flex stainless steel roof drain hose |
US6742815B2 (en) | 2002-05-08 | 2004-06-01 | Dormont Manufacturing Company | Fluid line connector assembly |
US20080283328A1 (en) * | 2007-05-18 | 2008-11-20 | International Truck Intellectual Property Company, Llc | Longitudinal stringer exhaust flex pipe assembly |
US7614475B2 (en) * | 2007-05-18 | 2009-11-10 | International Truck Intellectual Property Company, Llc | Longitudinal stringer exhaust flex pipe assembly |
US9273810B1 (en) * | 2012-02-14 | 2016-03-01 | Delafield Corporation | Metal hose fitting and flanged insert that safely conducts high velocity fluids/gases up to Mach 1 |
USD756872S1 (en) | 2014-11-20 | 2016-05-24 | Stauffer Diesel, Inc. | Exhaust pipe |
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